# @A300-600 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. ATA SYSTEM: 31 

### TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN 35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 13590S22843 13634S22870 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following reports of events of rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, a new Flight Warning Computer (FWC) standard S17 has been mainly developed to generate a new "STOP RUDDER INPUTS" synthetic voice audio warning associated with the detection of rudder reversal. This warning is generated by the Flight Control Computer (FCC). This Service Bulletin is issued to inform all operators of A300-600 aircraft of the issue of AIRBUS FRANCE Avionics and Simulation Products Service Bulletin No. 35-0B5-31-027. The modification consists in upgrading two FWC standard S15 PN 35-0B5-3006-318 installed by Mod. No. 13271S22526 (Service Bulletin No. A300-31-6135) in two FWC standard S17 PN 35-0B5-3008-320. Accomplishment of this Service Bulletin primarily incorporates the following evolutions to FWC software: - New synthetic voice "STOP RUDDER INPUTS": The purpose of this alert is to inform pilots of excessive rudder pedal inputs at high airspeeds. Conditions to generate this alert are triggered by the FCC. NOTE: When Service Bulletin No. A300-22-6054 Mod. No. 13592S22487, Service Bulletin No. A300-22-6055 Mod. No. 13593S22853, Service Bulletin No. A300-22-6056 Mod. No. 13591S22844 and Service Bulletin No. A300-31-6140 Mod. No. 13590S22843 and 13634S22870 are embodied, in case of excessive rudder pedal reversal inputs, visual and aural warnings are triggered in the cockpit. Accomplishment of this Service Bulletin further incorporates the following evolutions to FWC software: DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 1 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN SUMMARY - New Traffic Alert and Collision Avoidance System (TCAS) monitoring: . Creation of two new amber ECAM cautions logics: "NAV ADC TCAS FAULT", "NAV ADC TCAS STBY" and "* NAV ADC TCAS FAULT" secondary alert. . Creation of a new status logic: "TCAS INOP". . Provision for creation of a new memo by EFIS-Symbol Generator Units (SGU) ECAM: "TCAS STBY". The TCAS evolution requires the embodiment of a SGU ECAM standard W33. As a consequence, "TCAS INSTALLED" hard pin program should not be activated while aircraft is not fitted with a SGU ECAM able to support the display of TCAS messages. - Modification of ’fuel consumption increase’ logic to cover spoiler failure cases. - Improvement of FWC input test to avoid spurious fault triggering. - ROM LU1 margin memory increase. - Inhibition of the single chime associated to the "FUEL CTR TK L+R PUMPS LO PR" alert during phase 3. - Improvement of sound emission associated to the following ECAM alerts: . "CONFIG SLATS NOT IN T.O CONFIG" and "CONFIG FLAPS NOT IN T.O CONFIG" . "CONFIG SPD BRK NOT RETRACTED" and "CONFIG PITCH TRIM NOT IN T.O RANGE". . "ELEC BAT 1(2)(3) OVHT". . "FLT CTL FLAPS SYS 1+2 FAULT" and "FLT CTL FLAPS STUCK". . "FLT CTL SLATS SYS 1+2 FAULT" and "FLT CTL SLATS STUCK". . OVERSPEED red alerts. The operational consequences of this Service Bulletin are the modification of the Flight Crew Operating Manual (FCOM) and the Master Minimum Equipment List (MMEL). NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17. NOTE: For a full improvements description, refer to Modification Operational Impact (MOI) No.13590 and 13634. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED YES RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES
DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 2 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN SUMMARY NOTE (1) : Service Bulletin recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB FWC EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

34Z 77T 83V AAL ABD AHK AIB AMU BCS CES F2I FDX G8E GBG IRA IRM JAL KAC KAL MNB MON MSR MXU OHY QTR RUN SUD TAR THA TMA UPS URS UZB CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A300-31-6135 Mod. No. 13271S22526 REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD NO SOFT YES OBRM NO MANPOWER Task 316140-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to:
DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 3 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN SUMMARY Task 316140-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. Modify the two FWCs (FINs 1WW1 and 1WW2). AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027 Task 316140-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM. TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 APPENDICES None

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 4 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN SUMMARY

**CONF ALL

1WW1

1WW2

90VU FR1 FR20 Z120 

### A



## A

D_SB_316140_5_SAAA_01_00 Figure A-FSAAA - Sheet 01

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 5 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN SUMMARY

This Page Intentionally Left Blank

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 6 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 ATA SYSTEM: 31 

### TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN 35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING MODIFICATION No.: 13590S22843 13634S22870 This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY NOTE: These modifications are applicable by Service Bulletin only. (1) Models B4-603 B4-605R B4-620 B4-622 B4-622R C4-605R/FC4-620 F4-605R F4-622R (2) Effectivity by MSN 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0423 0459-0466 0469-0470 0474 0477 0479 0505-0518 0521 0525 0529-0530 0532 0536 0540 0543 0546 0553-0561 0563 0566 0569 0572 0575 0577 0579 0581-0582 0584 0602-0615 0617-0618 0621 0623 0625-0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721-0750 0752-0764 0766-0775 0777-0794 0797 0799-0841 0845-0878

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 1 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 34Z 0685 77T 0838 83V 0423 0459 0460 0463 0466 0470 0474 0510 0511 0512 0615 0639 0675 AAL 0517 0612 ABD 0529 0557 AHK 0855 0856 0857 0858 0859 0860 0870 0871 AIB 0507 0508 0515 AMU 0677 BCS 0621 0637 0641 0670 0679 0703 0711 0724 0729 0730 0737 0740 0753 0770 CES 0521 0525 0532 0707 0725 0732 0741 0746 0754 0763 F2I 0284 0294 0301 0307 0312 0317 0321 0336 0348 0351 0461 0518 0606 0610 0645 FDX 0358 0361 0365 0388 0417 0477 0479 0530 0536 0543 0555 0559 0572 0575 0579 0581 0611 0613 0625 0630 0633 0657 0659 0664 0668 0688 0709 0713 0715 0726 0728 0735 0736 0738 0742 0745 0748 0752 0757 0759 0760 0761 0766 0768 0769 0771 0772 0774 0777 0778 0779 0780 0781 0789 0790 0791 0792 0793 0794 0799 0800 0801 0802 0803 0804 0873 0874 0875 0876 0877 0878 G8E 0462 0465 0469 0506 0509 0513 0514 0516 GBG 0626 0643 IRA 0632 0696 0723 0727 IRM 0380 0401 0405 0408 0411 0414 0546 0553 0608 0618 0623 0701 0750 0762 0773 JAL 0602 0617 0683 0783 KAC 0344 0673 0694 0699 0719 0721 KAL 0582 0609 0627 0631 0662 0692 0731 MNB 0734 0739 0755 0756 0758 MON 0540 0556 0604 0605 MSR 0561 0607 MXU 0767 0788 0797 0836 0837 OHY 0584 0603 0744 0747 0749 0764 QTR 0554 0560 0614 RUN 0743 SUD 0666 0775 TAR 0505 0558 0563 THA 0464 0566 0569 0577 0628 0629 0635 0681 0705 0782 0784 0785 0786 0787 TMA 0872

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 2 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

OPERATOR MSN UPS 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0839 0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0861 0862 0863 0864 0865 0866 0867 0868 0869 URS 0733 UZB 0717 0722 (4) Configuration by MSN MSN CONFIGURATION 0284 0294 0301 0307 0312 0317 0321 0336 0344 0348 0351 0358 0361 0365 0380 0388 0401 0405 0408 0411 0414 0417 0423 0459 0460 0461 0462 0463 0464 0465 0466 0469 0470 0474 0477 0479 0505 0506 0507 0508 0509 0510 0511 0512 0513 0514 0515 0516 0517 0518 0521 0525 0529 0530 0532 0536 0540 0543 0546 0553 0554 0555 0556 0557 0558 0559 0560 0561 0563 0566 0569 0572 0575 0577 0579 0581 0582 0584 0602 0603 0604 0605 0606 0607 0608 0609 0610 0611 0612 0613 0614 0615 0617 0618 0621 0623 0625 0626 0627 0628 0629 0630 0631 0632 0633 0635 0637 0639 0641 0643 0645 0657 0659 0662 0664 0666 0668 0670 0673 0675 0677 0679 0681 0683 0685 0688 0692 0694 0696 0699 0701 0703 0705 0707 0709 0711 0713 0715 0717 0719 0721 0722 0723 0724 0725 0726 0727 0728 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743 0744 0745 0746 0747 0748 0749 0750 0752 0753 0754 0755 0756 0757 0758 0759 0760 0761 0762 0763 0764 0766 0767 0768 0769 0770 0771 0772 0773 0774 0775 0777 0778 0779 0780 0781 0782 0783 0784 0785 0786 0787 0788 0789 0790 0791 0792 0793 0794 0797 0799 0800 0801 0802 0803 0804 0805 0806 0807 0808 0809 0810 0811 0812 0813 0814 0815 0816 0817 0818 0819 0820 0821 0822 0823 0824 0825 0826 0827 0828 0829 0830 0831 0832 0833 0834 0835 0836 0837 0838 0839 0840 0841 0845 0846 0847 0848 0849 0850 0851 0852 0853 0854 0855 0856 0857 0858 0859 0860 0861 0862 0863 0864 0865 0866 0867 0868 0869 0870 0871 0872 0873 0874 0875 0876 0877 0878 001

(5) Configuration definition **CONF 001 Config. 001 is valid for all aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 3 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A300-31-6135 Mod. No. 13271S22526 C. REASON (1) History Following reports of events of rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, a new Flight Warning Computer (FWC) standard S17 has been mainly developed to generate a new "STOP RUDDER INPUTS" synthetic voice audio warning associated with the detection of rudder reversal. This warning is generated by the Flight Control Computer (FCC). (2) Objective/Action This Service Bulletin is issued to inform all operators of A300-600 aircraft of the issue of AIRBUS FRANCE Avionics and Simulation Products Service Bulletin No. 35-0B5-31-027. The modification consists in upgrading two FWC standard S15 PN 35-0B5-3006-318 installed by Mod. No. 13271S22526 (Service Bulletin No. A300-31-6135) in two FWC standard S17 PN 35-0B5-3008-320. (3) Advantages Accomplishment of this Service Bulletin primarily incorporates the following evolutions to FWC software: - New synthetic voice "STOP RUDDER INPUTS": The purpose of this alert is to inform pilots of excessive rudder pedal inputs at high airspeeds. Conditions to generate this alert are triggered by the FCC. NOTE: When Service Bulletin No. A300-22-6054 Mod. No. 13592S22487, Service Bulletin No. A300-22-6055 Mod. No. 13593S22853, Service Bulletin No. A300-22-6056 Mod. No. 13591S22844 and Service Bulletin No. A300-31-6140 Mod. No. 13590S22843 and 13634S22870 are embodied, in case of excessive rudder pedal reversal inputs, visual and aural warnings are triggered in the cockpit. Accomplishment of this Service Bulletin further incorporates the following evolutions to FWC software: - New Traffic Alert and Collision Avoidance System (TCAS) monitoring: . Creation of two new amber ECAM cautions logics: "NAV ADC TCAS FAULT", "NAV ADC TCAS STBY" and "* NAV ADC TCAS FAULT" secondary alert. . Creation of a new status logic: "TCAS INOP".

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 4 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN . Provision for creation of a new memo by EFIS-Symbol Generator Units (SGU) ECAM: "TCAS STBY". The TCAS evolution requires the embodiment of a SGU ECAM standard W33. As a consequence, "TCAS INSTALLED" hard pin program should not be activated while aircraft is not fitted with a SGU ECAM able to support the display of TCAS messages. - Modification of ’fuel consumption increase’ logic to cover spoiler failure cases. - Improvement of FWC input test to avoid spurious fault triggering. - ROM LU1 margin memory increase. - Inhibition of the single chime associated to the "FUEL CTR TK L+R PUMPS LO PR" alert during phase 3. - Improvement of sound emission associated to the following ECAM alerts: . "CONFIG SLATS NOT IN T.O CONFIG" and "CONFIG FLAPS NOT IN T.O CONFIG" . "CONFIG SPD BRK NOT RETRACTED" and "CONFIG PITCH TRIM NOT IN T.O RANGE". . "ELEC BAT 1(2)(3) OVHT". . "FLT CTL FLAPS SYS 1+2 FAULT" and "FLT CTL FLAPS STUCK". . "FLT CTL SLATS SYS 1+2 FAULT" and "FLT CTL SLATS STUCK". . OVERSPEED red alerts. (4) Operational/Maintenance Consequences The operational consequences of this Service Bulletin are the modification of the Flight Crew Operating Manual (FCOM) and the Master Minimum Equipment List (MMEL). NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17. NOTE: For a full improvements description, refer to Modification Operational Impact (MOI) No.13590 and 13634. D. DESCRIPTION NOTE: To accomplish this Service Bulletin, two possibilities are available: - Either modify the two FWCs (FINs 1WW1 and 1WW2) as described in TASK 316140-831-801 001 Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. - Or replace them as described in TASK 316140-831-802 001 Modification by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM. DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 5 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN To accomplish this Service Bulletin it is necessary to : Task 316140-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. (1) In the Electronics Rack 90VU, remove the two FWCs (FINs 1WW1 and 1WW2). (2) Modify the two FWCs (FINs 1WW1 and 1WW2). (3) In the Electronics Rack 90VU, install the two FWCs (FINs 1WW1 and 1WW2). Task 316140-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM. (1) In the Electronics Rack 90VU, replace the two FWCs (FINs 1WW1 and 1WW2). E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL The technical content of this document is approved under the authority of Design Organization Approval No. EASA.21J.031. If an aircraft listed in the effectivity has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin. G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included. Task 316140-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. Get Access 0.50 On Aircraft In the Electronics Rack 90VU, remove the two FWCs (FINs 1WW1 and 1WW2). 0.50

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 6 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN
Task 316140-831-801-001: Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. In the Electronics Rack 90VU, install the two FWCs (FINs 1WW1 and 1WW2). 0.50 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to: Modify the two FWCs (FINs 1WW1 and 1WW2). AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027 Task 316140-831-802-001: Modification by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM. Get Access 0.50 On Aircraft In the Electronics Rack 90VU, replace the two FWCs (FINs 1WW1 and 1WW2). 1.00 Tests 0.50 Close-Up 0.50 TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 24-00-00 31-53-34 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Modification Operational Impact (MOI) 13590 13634 Service Bulletin (SB) A300-31-6135 Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027 K. PUBLICATION AFFECTED

Aircraft Wiring List (AWL) Flight Crew Operating Manual (FCOM) Illustrated Parts Catalog (IPC) 31-53-08 DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 7 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN
Master Minimum Equipment List (MMEL) This Service Bulletin has an operational impact. Please inform AIRBUS, at least four weeks in advance, in case you need your operational documentation to be amended by a revision priorto Service Bulletin embodiment. For this purpose, please request the revision by e-mail, online through the SB Reporting service or alternatively by fax to: SEDOR4 - AIRBUS Customer Services Technical Data Fax No: (33) 5 61 93 28 06 E-mail: sb.reporting@airbus.com SB Reporting service is accessible on-line through AIRBUSWorld from: My on-line services’ section, available on all AIRBUSWorld pages. The Maintenance and Engineering Community, in: - Modify and Upgrade page, - Access SB and VSB section. These amendments will be confirmed by the next normal revision of operational documentation, once your Service Bulletin accomplishment report has been sent, as usual, to our Customer Services Aircraft In-Service Data (SEDOR4). NOTE: MMEL is affected if SGU ECAM W33 is installed with FWC S17. L. INTERCHANGEABILITY/MIXABILITY DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FWC 35-0B5-3008-318 35-0B5-3008-320 03 NO (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1) : Mixability not authorized. Replacement of the two old FWCs has to be done as a set. M. SPARES FWC 35-0B5-3008-318

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 8 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Equipment BFEA01 The material is included in the commercial offer of the Letter Agreement, and as such will be supplied by AIRBUS Upgrade Services. Airline Customers are requested to contact: AIRBUS Upgrade Services Attn KAM Manager (2) Price and Availability Sales terms must be agreed between the Customer and AIRBUS in accordance with the RFC (or RFC/RMO) procedure in the framework of the Stop Rudder Inputs Warning retrofit. B. INDUSTRY SUPPORT INFORMATION Refer to the paragraph: ’Price and Availability’. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components None (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 35-0B5-3008-320 2 FWC 35-0B5-3008-318 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.
DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 9 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 10 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 316140-831-801-001 - Modification of the two FWCs (FINs 1WW1 and 1WW2) by Vendor AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 120 Modified FIN 1WW1 1WW2 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 Additional manhours related to Vendor SB; refer to: AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027 A. GENERAL (1) Subtask 316140-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin.

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 11 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

B. PREPARATION (1) Subtask 316140-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 31-53-34, Page Block 401 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Do the Job Set-up procedure as specified in the removal of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). C. PROCEDURE (1) Subtask 316140-831-001-001 - In the Electronics Rack 90VU, remove the two FWCs (FINs 1WW1 and 1WW2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Remove: Refer to AMM 31-53-34, Page Block 401 FIN 1WW1 1 FWC 35-0B5-3008-318 and FIN 1WW2 1 FWC 35-0B5-3008-318

(2) Subtask 316140-831-002-001 - Modify the two FWCs (FINs 1WW1 and 1WW2). References Vendor Service Bulletin (VSB) AIRBUS FRANCE SAS 35-0B5-31-027 DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 12 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN (a) Modify the two FWCs (FINs 1WW1 and 1WW2) as per instructions given in AIRBUS FRANCE SAS Service Bulletin No. 35-0B5-31-027. (3) Subtask 316140-831-003-001 - In the Electronics Rack 90VU, install the two FWCs (FINs 1WW1 and 1WW2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 35-0B5-3008-320 2 FWC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Install: Refer to AMM 31-53-34, Page Block 401 FIN 1WW1 1 FWC 35-0B5-3008-320 and FIN 1WW2 1 FWC 35-0B5-3008-320 D. TEST (1) Subtask 316140-700-001-001 - Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Remove the safety clips and/or tags and close/unlock the circuit breakers as specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 13 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN (b) Do the test procedure as specified after the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). E. CLOSE-UP (1) Subtask 316140-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). (c) Restore the systems and the aircraft to normal operating condition.

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 14 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN Task 316140-831-802-001 - Modification by replacement of the two FWCs (FINs 1WW1 and 1WW2) as per AMM. WARNING: MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC; AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 120 Modified FIN 1WW1 1WW2 Manpower TOTAL MANHOURS 2.50 ELAPSED TIME (HOURS) 2.50 A. GENERAL (1) Subtask 316140-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 316140-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 15 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 31-53-34, Page Block 401 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Do the Job Set-up procedure as specified in the removal of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). C. PROCEDURE (1) Subtask 316140-960-001-001 - In the Electronics Rack 90VU, replace the two FWCs (FINs 1WW1 and 1WW2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 35-0B5-3008-320 2 FWC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Remove: Refer to AMM 31-53-34, Page Block 401 FIN 1WW1 1 FWC 35-0B5-3008-318 and FIN 1WW2 1 FWC 35-0B5-3008-318 (b) Install: Refer to AMM 31-53-34, Page Block 401
DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 16 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN

FIN 1WW1 1 FWC 35-0B5-3008-320 and FIN 1WW2 1 FWC 35-0B5-3008-320 D. TEST (1) Subtask 316140-700-002-001 - Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Remove the safety clips and/or tags and close/unlock the circuit breakers as specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). (b) Do the test procedure as specified after the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). E. CLOSE-UP (1) Subtask 316140-942-002-002 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-53-34, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified in the installation of the two FWCs (FINs 1WW1 and 1WW2) (Refer to AMM 31-53-34, Page Block 401). (c) Restore the systems and the aircraft to normal operating condition.

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 17 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN REPORTING SHEET 

### TITLE: INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC PN 35-0B5-3008-320 CAPABLE OF RUDDER INPUT WARNING MODIFICATION No.: 13590S22843 13634S22870 Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:

From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 1 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A300-600 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - Is this SB easy to understand ? Y/N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: May 04/12 SERVICE BULLETIN No.: A300-31-6140 REVISION No.: 00 - May 04/12 Page: 1 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.